Design of a Third-Generation Boundary Layer Measurement System-Reference-Cited by-同舟云学术

Design of a Third-Generation Boundary Layer Measurement System

Published:2008-06-14 Issue: Volume: Page:
ISSN:
Container-title:26th AIAA Applied Aerodynamics Conference
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Author:

Westphal Russ¹,Frame Donald¹,Jordan Steven¹,Wanner Arthur¹,Thompson Bryce¹,Bender Anne²,Drake Aaron³

Affiliation:

1. Washington State University

2. Northrop Grumman Corp.

3. Northrop Grumman Corp

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-7332

Reference11 articles.

1. 1Marshall, L. A. "Boundary-Layer Transition Results From the F-16XL Supersonic Laminar Flow Control Experiment," NASA TM-1999-209013,1999.

2. 2Stuper,J."InvestigationofBoundaryLayersonanAirplaneWinginFreeFlight,"NACATM751,1934.

3. 3Bui, T. T., Oates, B. L., and Gonzalez, J. C. "Design and Evaluation of a New Boundary-Layer Rake for Flight Testing," NASA TM-2000-209014,2000.

4. 5Bleazard,M."AResearchInstrumentforBoundaryLayerMeasurementsinFlight,"M.S.Thesis,SchoolofMechanicaland Materials Engineering, WashingtonStateUniv.,Pullman, WA, 2006.

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